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The Effect of Journal Roughness and Foil Coatings on the Performance of Heavily Loaded Foil Air Bearings

机译:轴颈粗糙度和箔涂层对大装载箔空气轴承性能的影响

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Foil air bearing load capacity tests were conducted to investigate if a solid lubricant coating applied to the surface of the bearing's top foil can function as a break-in coating. Two foil coating materials, a conventional soft polymer film (polyimide) and a hard ceramic (alumina), were independently evaluated against as-ground and worn (run-in) journals coated with NASA P5304, a high-temperature solid lubricant composite coating. The foil coatings were evaluated at journal rotational speeds of 30000 rpm and at 25°C. Tests were also performed on a toil bearing with a bare (uncoated) nickel-based superalloy top foil to establish a baseline for comparison. The test results indicate that the presence of a top foil solid lubricant coating is effective at increasing the load capacity performance of the foil bearing. Compared to the uncoated baseline, the addition of the soft polymer coating on the top foil increased the bearing load coefficient by 120% when operating against an as-ground journal surface and 85% against a run-in journal surface. The alumina coating increased the load coefficient by 40% against the as-ground journal but did not have any affect when the bearing was operated with the run-in journal. The results suggest that the addition of solid lubricant films provide added lubrication when the air film is marginal indicating that as the load capacity is approached foil air bearings transition from hydrodynamic to mixed and boundary lubrication.
机译:进行箔空气轴承负载能力测试以研究施加到轴承顶部箔的表面的固体润滑剂涂层可以用作碎裂涂层。两个箔涂料,常规的软聚合物膜(聚酰亚胺)和硬陶瓷(氧化铝),独立地针对涂覆有NASA P5304,高温固体润滑剂复合涂层的地面和覆盖(in)磨损(挤出)轴颈。在30000rpm和25℃下以30000rpm的速度旋转速度评估箔涂层。还在用裸露(未涂覆的)镍基超合金顶部箔上进行试验,以建立基线进行比较。试验结果表明,顶部箔固体润滑剂涂层的存在在增加箔轴承的负载能力性能方面是有效的。与未涂层的基线相比,当对逆合轴颈表面和85%逆合轴颈表面进行操作时,在顶部箔上加入轴上箔上的软聚合物涂层将轴承载荷系数增加120%。氧化铝涂层将负荷系数增加40%,抵抗AS-地轴颈,但当轴承与载流运行时没有任何影响。结果表明,当空气膜是边缘表示的情况下,添加固体润滑膜的添加提供了添加的润滑,表明随着负载能力接近从流体动力到混合和边界润滑的箔空气轴承过渡。

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